EP 2957975 B1 20180502 - METHOD AND DEVICE FOR CONTROLLING AT LEAST ONE ACTUATOR CONTROL SYSTEM OF AN AIRCRAFT, RELATED COMPUTER PROGRAM PRODUCT AND AIRCRAFT
Title (en)
METHOD AND DEVICE FOR CONTROLLING AT LEAST ONE ACTUATOR CONTROL SYSTEM OF AN AIRCRAFT, RELATED COMPUTER PROGRAM PRODUCT AND AIRCRAFT
Title (de)
STEUERVERFAHREN UND -VORRICHTUNG MINDESTENS EINES KONTROLLSYSTEMS EINES STELLGLIEDS EINES LUFTFAHRZEUGS, ENTSPRECHENDES COMPUTERPROGRAMM-PRODUKT UND ENTSPRECHENDES LUFTFAHRZEUG
Title (fr)
PROCÉDÉ ET DISPOSITIF DE COMMANDE D'AU MOINS UN SYSTÈME DE CONTRÔLE D'ACTIONNEUR D'UN AÉRONEF, PRODUIT PROGRAMME D'ORDINATEUR ET AÉRONEF ASSOCIÉS
Publication
Application
Priority
FR 1401358 A 20140616
Abstract (en)
[origin: CA2889433A1] This method provides ability to control an actuator control system of an aircraft for acting on a force applied to the aircraft. The aircraft has an air speed vector and a ground speed vector, and comprises an engine and an engine control system, forming a first actuator control system, for causing the varying of a thrust force generated by the engine. The method comprises determination of a thrust variation for controlling a variable relating to the aircraft relative to a set point, and calculation of a first control command signal to be sent to the engine control system in order to obtain said thrust variation, and transmission of said first control command signal to said engine control system. The controlled variable is an acceleration along a direction of a speed vector among the air and ground speed vectors, and the set point is an acceleration set point along said direction.
IPC 8 full level
B64D 31/06 (2006.01); G01C 23/00 (2006.01)
CPC (source: EP US)
B64C 25/44 (2013.01 - US); B64D 31/06 (2013.01 - EP US); B64D 33/04 (2013.01 - US); G01C 23/00 (2013.01 - EP US)
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
DOCDB simple family (publication)
EP 2957975 A1 20151223; EP 2957975 B1 20180502; BR 102015012254 A2 20161018; CA 2889433 A1 20151216; FR 3022355 A1 20151218; FR 3022355 B1 20180330; US 2015360789 A1 20151217; US 9856032 B2 20180102
DOCDB simple family (application)
EP 15168729 A 20150521; BR 102015012254 A 20150527; CA 2889433 A 20150429; FR 1401358 A 20140616; US 201514729509 A 20150603